Heat treatable L12 aluminum alloys

ABSTRACT

High temperature heat treatable aluminum alloys that can be used at temperatures from about −420° F. (−251° C.) up to about 650° F. (343° C.) are described. The alloys are strengthened by dispersion of particles based on the L1 2  intermetallic compound Al 3 X. These alloys comprise aluminum, copper, magnesium, at least one of scandium, erbium, thulium, ytterbium, and lutetium; and at least one of gadolinium, yttrium, zirconium, titanium, hafnium, and niobium. Lithium is an optional alloying element.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application is related to the following co-pending applicationsthat are filed on even date herewith and are assigned to the sameassignee: L1₂ ALUMINUM ALLOYS WITH BIMODAL AND TRIMODAL DISTRIBUTION,Ser. No. _______, Attorney Docket No. PA0006933U-U73.12-325KL;DISPERSION STRENGTHENED L1₂ ALUMINUM ALLOYS, Ser. No. ______, AttorneyDocket No. PA0006932U-U73.12-326KL; HEAT TREATABLE L1₂ ALUMINUM ALLOYS,Ser. No. ______, Attorney Docket No. PA0006931U-U73.12-327KL; HIGHSTRENGTH L1₂ ALUMINUM ALLOYS, Ser. No. ______, Attorney Docket No.PA0006929U-U73.12-329KL; HIGH STRENGTH L1₂ ALUMINUM ALLOYS, Ser. No.______, Attorney Docket No. PA0006928U-U73.12-330KL; HIGH STRENGTH L1₂ALUMINUM ALLOYS, Ser. No. ______, Attorney Docket No.PA0006926U-U73.12-332KL; HIGH STRENGTH ALUMINUM ALLOYS WITH L1₂PRECIPITATES, Ser. No. ______, Attorney Docket No.PA0006924U-U73.12-334KL; HIGH STRENGTH L1₂ ALUMINUM ALLOYS, Ser. No.______, Attorney Docket No. PA0006923U-U73.12-335KL; and L1₂STRENGTHENED AMORPHOUS ALUMINUM ALLOYS, Ser. No. ______, Attorney DocketNo. PA0001359U-U73.12-336KL.

BACKGROUND

The present invention relates generally to aluminum alloys and morespecifically to heat treatable aluminum alloys produced by meltprocessing and strengthened by L1₂ phase dispersions.

The combination of high strength, ductility, and fracture toughness, aswell as low density, make aluminum alloys natural candidates foraerospace and space applications. However, their use is typicallylimited to temperatures below about 300° F. (149° C.) since mostaluminum alloys start to lose strength in that temperature range as aresult of coarsening of strengthening precipitates.

The development of aluminum alloys with improved elevated temperaturemechanical properties is a continuing process. Some attempts haveincluded aluminum-iron and aluminum-chromium based alloys such asAl—Fe—Ce, Al—Fe—V—Si, Al—Fe—Ce—W, and Al—Cr—Zr—Mn that containincoherent dispersoids. These alloys, however, also lose strength atelevated temperatures due to particle coarsening. In addition, thesealloys exhibit ductility and fracture toughness values lower than othercommercially available aluminum alloys.

Other attempts have included the development of mechanically alloyedAl—Mg and Al—Ti alloys containing ceramic dispersoids. These alloysexhibit improved high temperature strength due to the particledispersion, but the ductility and fracture toughness are not improved.

U.S. Pat. No. 6,248,453 discloses aluminum alloys strengthened bydispersed Al₃X L1₂ intermetallic phases where X is selected from thegroup consisting of Sc, Er, Lu, Yb, Tm, and U. The Al₃X particles arecoherent with the aluminum alloy matrix and are resistant to coarseningat elevated temperatures. The improved mechanical properties of thedisclosed dispersion strengthened L1₂ aluminum alloys are stable up to572° F. (300° C.). In order to create aluminum alloys containing finedispersions of Al₃X L1₂ particles, the alloys need to be manufactured byexpensive rapid solidification processes with cooling rates in excess of1.8×10³ F/sec (10³° C./sec). U.S. Patent Application Publication No.2006/0269437 A1 discloses an aluminum alloy that contains scandium andother elements. While the alloy is effective at high temperatures, it isnot capable of being heat treated using a conventional age hardeningmechanism.

Heat treatable aluminum alloys strengthened by coherent L1₂intermetallic phases produced by standard, inexpensive melt processingtechniques would be useful.

SUMMARY

The present invention is heat treatable aluminum alloys that can becast, wrought, or formed by rapid solidification, and thereafter heattreated. The alloys can achieve high temperature performance and can beused at temperatures up to about 650° F. (343° C.).

These alloys comprise copper, magnesium, lithium and an Al₃X L1₂dispersoid where X is at least one first element selected from scandium,erbium, thulium, ytterbium, and lutetium, and at least one secondelement selected from gadolinium, yttrium, zirconium, titanium, hafnium,and niobium. The balance is substantially aluminum.

The alloys have less than about 1.0 weight percent total impurities.

The alloys are formed by a process selected from casting, deformationprocessing and rapid solidification. The alloys are then heat treated ata temperature of from about 900° F. (482° C.) to about 1100° F. (593°C.) for between about 30 minutes and four hours, followed by quenchingin water, and thereafter aged at a temperature from about 200° F. (93°C.) to about 600° F. (315° C.) for about two to about forty-eight hours.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is an aluminum copper phase diagram.

FIG. 2 is an aluminum magnesium phase diagram.

FIG. 3 is an aluminum lithium phase diagram.

FIG. 4 is an aluminum scandium phase diagram.

FIG. 5 is an aluminum erbium phase diagram.

FIG. 6 is an aluminum thulium phase diagram.

FIG. 7 is an aluminum ytterbium phase diagram.

FIG. 8 is an aluminum lutetium phase diagram.

DETAILED DESCRIPTION

The alloys of this invention are based on the aluminum, copper,magnesium, lithium system. The amount of copper in these alloys rangesfrom about 1.0 to about 8.0 weight percent, more preferably about 2.0 toabout 7.0 weight percent, and even more preferably about 3.5 to about6.5 weight percent. The amount of magnesium in these alloys ranges fromabout 0.2 to about 4.0 weight percent, more preferably about 0.4 toabout 3.0 weight percent, and even more preferably about 0.5 to about2.0 weight percent. The amount of lithium in these alloys ranges fromabout 0.5 to about 3.0 weight percent, more preferably about 1.0 toabout 2.5 weight percent, and even more preferably about 1.0 to about2.0 weight percent.

Copper, magnesium and lithium are completely soluble in the compositionof the inventive alloys discussed herein. Aluminum magnesium lithiumalloys are heat treatable with L1₂ Al₃Li (δ′), Al₂LiMg, Al₂CuMg (S′) andAl₂CuLi precipitating following a solution heat treatment, quench andage process. These phases precipitate as coherent second phases in thealuminum magnesium lithium solid solution matrix. Also, in the solidsolutions are dispersions of Al₃X having an L1₂ structure where X is atleast one first element selected from scandium, erbium, thulium,ytterbium, and lutetium and at least one second element selected fromgadolinium, yttrium, zirconium, titanium, hafnium, and niobium.

The aluminum copper phase diagram is shown in FIG. 1. The aluminumcopper binary system is a eutectic alloy system with a eutectic reactionat 31.2 weight percent magnesium and 1018° F. (548.2° C.). Copper hasmaximum solid solubility of 6 weight percent in aluminum at 1018° F.(548.2° C.) which can be extended further by rapid solidificationprocessing. Copper provides a considerable amount of precipitationstrengthening in aluminum by precipitation of fine second phases. Thepresent invention is focused on hypoeutectic alloy composition ranges.

The aluminum magnesium phase diagram is shown in FIG. 2. The binarysystem is a eutectic alloy system with a eutectic reaction at 36 weightpercent magnesium and 842° F. (450° C.). Magnesium has maximum solidsolubility of 16 weight percent in aluminum at 842° F. (450° C.) whichcan be extended further by rapid solidification processing. Magnesiumprovides substantial solid solution strengthening in aluminum. Inaddition, magnesium provides precipitation strengthening throughprecipitation of Al₂CuMg (S′) phase in the presence of copper.

The aluminum lithium phase diagram is shown in FIG. 3. The binary systemis a eutectic alloy system with a eutectic reaction at 8 weight percentmagnesium and 1104° F. (596° C.). Lithium has maximum solid solubilityof about 4.5 weight percent in aluminum at 1104° F. (596° C.). Lithiumhas lesser solubility in aluminum in the presence of magnesium comparedto when magnesium is absent. Therefore, lithium provides significantprecipitation strengthening through precipitation of Al₃Li (δ′) phase.Lithium in addition provides reduced density and increased modulus inaluminum. In the presence of magnesium and copper, lithium forms ternaryprecipitates based on Al₂CuLi and Al₂MgLi.

The alloys of this invention contain phases consisting of primaryaluminum, aluminum copper solid solutions, aluminum magnesium solidsolutions, and aluminum lithium solid solutions. In the solid solutionsare dispersions of Al₃X having an L1₂ structure where X is at least oneelement selected from scandium, erbium, thulium, ytterbium, andlutetium. Also present is at least one element selected from gadolinium,yttrium, zirconium, titanium, hafnium, and niobium. Exemplary aluminumalloys of this invention include, but are not limited to (in weightpercent):

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-0.5)Sc-(0.1-4.0)Gd;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-6)Er-(0.1-4.0)Gd;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-10)Tm-(0.1-4.0)Gd;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-15)Yb-(0.1-4.0)Gd;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-12)Lu-(0.1-4.0)Gd;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-0.5)Sc-(0.1-4.0)Y;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-6)Er-(0. 1-4.0)Y;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-10)Tm-(0.1-4.0)Y;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-15)Yb-(0.1-4.0)Y;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-12)Lu-(0.1-4.0)Y;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-0.5)Sc-(0.05-1.0)Zr;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-6)Er-(0.05-1.0)Zr;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-10)Tm-(0.05-1.0)Zr;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-15)Yb-(0.05-1.0)Zr;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-12)Lu-(0.05-1.0)Zr;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-0.5)Sc-(0.05-2.0)Ti;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-0.5)Er-(0.05-2.0)Ti;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-10)Tm-(0.05-2.0)Ti;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-15)Yb-(0.05-2.0)Ti;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-4)-Lu-(0.05-2.0)Ti;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-0.5)Sc-(0.05-2.0)Hf;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-6)Er-(0.05-2.0)Hf;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-10)Tm-(0.05-2.0)Hf;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-15)Yb-(0.05-2.0)Hf;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-12)Lu-(0.05-2.0)Hf;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-0.5)Sc-(0.05-1.0)Nb;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-6)Er-(0.05-1.0)Nb;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-10)Tm-(0.05-1.0)Nb;

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-15)Yb-(0.05-1.0)Nb; and

Al-(1-8)Cu-(0.2-4)Mg-(0.5-3.0)Li-(0.1-12)Lu-(0.05-1.0)Nb.

Preferred examples of similar alloys to these are alloys with about 2.0to about 7.0 weight percent copper, alloys with about 0.4 to about 3.0weight percent magnesium, and alloys with about 1.0 to about 2.5 weightpercent lithium.

In the inventive aluminum based alloys disclosed herein, scandium,erbium, thulium, ytterbium, and lutetium are potent strengtheners thathave low diffusivity and low solubility in aluminum. All these elementform equilibrium Al₃X intermetallic dispersoids where X is at least oneof scandium, erbium, ytterbium, lutetium, that have an L1₂ structurethat is an ordered face centered cubic structure with the X atomslocated at the comers and aluminum atoms located on the cube faces ofthe unit cell.

Scandium forms Al₃Sc dispersoids that are fine and coherent with thealuminum matrix. Lattice parameters of aluminum and Al₃Sc are very close(0.405 nm and 0.410 nm respectively), indicating that there is minimalor no driving force for causing growth of the Al₃Sc dispersoids. Thislow interfacial energy makes the Al₃Sc dispersoids thermally stable andresistant to coarsening up to temperatures as high as about 842° F.(450° C.). In the alloys of this invention these Al₃Sc dispersoids aremade stronger and more resistant to coarsening at elevated temperaturesby adding suitable alloying elements such as gadolinium, yttrium,zirconium, titanium, hafnium, niobium, or combinations thereof, thatenter Al₃Sc in solution. Erbium forms Al₃Er dispersoids in the aluminummatrix that are fine and coherent with the aluminum matrix. The latticeparameters of aluminum and Al₃Er are close (0.405 nm and 0.417 nmrespectively), indicating there is minimal driving force for causinggrowth of the Al₃Er dispersoids. This low interfacial energy makes theAl₃Er dispersoids thermally stable and resistant to coarsening up totemperatures as high as about 842° F. (450° C.). Additions of magnesiumin solid solution in aluminum increase the lattice parameter of thealuminum matrix, and decrease the lattice parameter mismatch furtherincreasing the resistance of the Al₃Er to coarsening. Additions ofcopper increase the strength of alloys through precipitation of Al₂Cu(θ′) and Al₂CuMg (S′) phases. In the alloys of this invention, theseAl₃Er dispersoids are made stronger and more resistant to coarsening atelevated temperatures by adding suitable alloying elements such asgadolinium, yttrium, zirconium, titanium, hafnium, niobium, orcombinations thereof that enter Al₃Er in solution.

Thulium forms metastable Al₃Tm dispersoids in the aluminum matrix thatare fine and coherent with the aluminum matrix. The lattice parametersof aluminum and Al₃Tm are close (0.405 nm and 0.420 nm respectively),indicating there is minimal driving force for causing growth of theAl₃Tm dispersoids. This low interfacial energy makes the Al₃Tmdispersoids thermally stable and resistant to coarsening up totemperatures as high as about 842° F. (450° C.). Additions of magnesiumin solid solution in aluminum increase the lattice parameter of thealuminum matrix, and decrease the lattice parameter mismatch furtherincreasing the resistance of the Al₃Tm to coarsening. Additions ofcopper increase the strength of alloys through precipitation of Al₂Cu(θ′) and Al₂CuMg (S′) phases. In the alloys of this invention theseAl₃Tm dispersoids are made stronger and more resistant to coarsening atelevated temperatures by adding suitable alloying elements such asgadolinium, yttrium, zirconium, titanium, hafnium, niobium, orcombinations thereof that enter Al₃Tm in solution.

Ytterbium forms Al₃Yb dispersoids in the aluminum matrix that are fineand coherent with the aluminum matrix. The lattice parameters of Al andAl₃Yb are close (0.405 nm and 0.420 nm respectively), indicating thereis minimal driving force for causing growth of the Al₃Yb dispersoids.This low interfacial energy makes the Al₃Yb dispersoids thermally stableand resistant to coarsening up to temperatures as high as about 842° F.(450° C.). Additions of magnesium in solid solution in aluminum increasethe lattice parameter of the aluminum matrix, and decrease the latticeparameter mismatch further increasing the resistance of the Al₃Yb tocoarsening. Additions of copper increase the strength of alloys throughprecipitation of Al₂Cu (θ′) and Al₂CuMg (S′) phases. In the alloys ofthis invention, these Al₃Yb dispersoids are made stronger and moreresistant to coarsening at elevated temperatures by adding suitablealloying elements such as gadolinium, yttrium, zirconium, titanium,hafnium, niobium, or combinations thereof that enter Al₃Yb in solution.

Lutetium forms Al₃Lu dispersoids in the aluminum matrix that are fineand coherent with the aluminum matrix. The lattice parameters of Al andAl₃Lu are close (0.405 nm and 0.419 nm respectively), indicating thereis minimal driving force for causing growth of the Al₃Lu dispersoids.This low interfacial energy makes the Al₃Lu dispersoids thermally stableand resistant to coarsening up to temperatures as high as about 842° F.(450° C.). Additions of magnesium in solid solution in aluminum increasethe lattice parameter of the aluminum matrix, and decrease the latticeparameter mismatch further increasing the resistance of the Al₃Lu tocoarsening. Additions of copper increase the strength of alloys throughprecipitation of Al₂Cu (θ′) and Al₂CuMg (S′) phases. In the alloys ofthis invention, these Al₃Lu dispersoids are made stronger and moreresistant to coarsening at elevated temperatures by adding suitablealloying elements such as gadolinium, yttrium, zirconium, titanium,hafnium, niobium, or mixtures thereof that enter Al₃Lu in solution.

Gadolinium forms metastable Al₃Gd dispersoids in the aluminum matrixthat are stable up to temperatures as high as about 842° F. (450° C.)due to their low diffusivity in aluminum. The Al₃Gd dispersoids have aD0₁₉ structure in the equilibrium condition. Despite its large atomicsize, gadolinium has fairly high solubility in the Al₃X intermetallicdispersoids (where X is scandium, erbium, thulium, ytterbium orlutetium). Gadolinium can substitute for the X atoms in Al₃Xintermetallic, thereby forming an ordered L1₂ phase which results inimproved thermal and structural stability.

Yttrium forms metastable Al₃Y dispersoids in the aluminum matrix thathave an L1₂ structure in the metastable condition and a D0₁₉ structurein the equilibrium condition. The metastable Al₃Y dispersoids have a lowdiffusion coefficient which makes them thermally stable and highlyresistant to coarsening. Yttrium has a high solubility in the Al₃Xintermetallic dispersoids allowing large amounts of yttrium tosubstitute for X in the Al₃X L1₂ dispersoids which results in improvedthermal and structural stability.

Zirconium forms Al₃Zr dispersoids in the aluminum matrix that have anL1₂ structure in the metastable condition and D0₂₃ structure in theequilibrium condition. The metastable Al₃Zr dispersoids have a lowdiffusion coefficient which makes them thermally stable and highlyresistant to coarsening. Zirconium has a high solubility in the Al₃Xdispersoids allowing large amounts of zirconium to substitute for X inthe Al₃X dispersoids, which results in improved thermal and structuralstability.

Titanium forms Al₃Ti dispersoids in the aluminum matrix that have an L1₂structure in the metastable condition and D0₂₂ structure in theequilibrium condition. The metastable Al₃Ti despersoids have a lowdiffusion coefficient which makes them thermally stable and highlyresistant to coarsening. Titanium has a high solubility in the Al₃Xdispersoids allowing large amounts of titanium to substitute for X inthe Al₃X dispersoids, which result in improved thermal and structuralstability.

Hafnium forms metastable Al₃Hf dispersoids in the aluminum matrix thathave an L1₂ structure in the metastable condition and a D0₂₃ structurein the equilibrium condition. The Al₃Hf dispersoids have a low diffusioncoefficient, which makes them thermally stable and highly resistant tocoarsening. Hafnium has a high solubility in the Al₃X dispersoidsallowing large amounts of hafnium to substitute for scandium, erbium,thulium, ytterbium, and lutetium in the above mentioned Al₃Xdispersoides, which results in stronger and more thermally stabledispersoids.

Niobium forms metastable Al₃Nb dispersoids in the aluminum matrix thathave an L1₂ structure in the metastable condition and a D0₂₂ structurein the equilibrium condition. Niobium has a lower solubility in the Al₃Xdispersoids than hafnium or yttrium, allowing relatively lower amountsof niobium than hafnium or yttrium to substitute for X in the Al₃Xdispersoids. Nonetheless, niobium can be very effective in slowing downthe coarsening kinetics of the Al₃X dispersoids because the Al₃Nbdispersoids are thermally stable. The substitution of niobium for X inthe above mentioned Al₃X dispersoids results in stronger and morethermally stable dispersoids.

Al₃X L1₂ precipitates improve elevated temperature mechanical propertiesin aluminum alloys for two reasons. First, the precipitates are orderedintermetallic compounds. As a result, when the particles are sheared byglide dislocations during deformation, the dislocations separate intotwo partial dislocations separated by an anti-phase boundary on theglide plane. The energy to create the anti-phase boundary is the originof the strengthening. Second, the cubic L1₂ crystal structure andlattice parameter of the precipitates are closely matched to thealuminum solid solution matrix. This results in a lattice coherency atthe precipitate/matrix boundary that resists coarsening. The lack of aninterphase boundary results in a low driving force for particle growthand resulting elevated temperature stability. Alloying elements in solidsolution in the dispersed strengthening particles and in the aluminummatrix that tend to decrease the lattice mismatch between the matrix andparticles will tend to increase the strengthening and elevatedtemperature stability of the alloy.

Copper has considerable solubility in aluminum at 1018° F. (548.2° C.),which decreases with a decrease in temperature. The aluminum copperalloy system provides considerable precipitation hardening responsethrough precipitation of Al₂Cu (θ′) second phase. Magnesium hasconsiderable solubility in aluminum at 842° F. (450° C.) which decreaseswith a decrease in temperature. The aluminum magnesium binary alloysystem does not provide precipitation hardening, rather it providessubstantial solid solution strengthening. When magnesium is added toaluminum copper alloy, it increases the precipitation hardening responseof the alloy considerably through precipitation of Al₂CuMg (S′) phase.When the ratio of copper to magnesium is high, precipitation hardeningoccurs through precipitation of GP zones through coherent metastableAl₂Cu (θ′) to equilibrium Al₂Cu (θ) phase. When the ratio of copper tomagnesium is low, precipitation hardening occurs through precipitationof GP zones through coherent metastable Al₂CuMg (S′) to equilibriumAl₂CuMg (S) phase. Lithium provides considerable strengthening throughprecipitation of coherent Al₃Li (δ′) phase. Lithium also forms Al₂MgLiand Al₂CuLi phases which provide additional strengthening whenprecipitated in desired size and shape. In addition, lithium reducesdensity and increases modulus of the aluminum alloys due to its lowerdensity and higher modulus.

The amount of scandium present in the alloys of this invention if anymay vary from about 0.1 to about 0.5 weight percent, more preferablyfrom about 0.1 to about 0.35 weight percent, and even more preferablyfrom about 0.1 to about 0.25 weight percent. The Al—Sc phase diagramshown in FIG. 4 indicates a eutectic reaction at about 0.5 weightpercent scandium at about 1219° F. (659° C.) resulting in a solidsolution of scandium and aluminum and Al₃Sc dispersoids. Aluminum alloyswith less than 0.5 weight percent scandium can be quenched from the meltto retain scandium in solid solution that may precipitate as dispersedL1₂ intermetallic Al₃Sc following an aging treatment. Alloys withscandium in excess of the eutectic composition (hypereutectic alloys)can only retain scandium in solid solution by rapid solidificationprocessing (RSP) where cooling rates are in excess of about 10³°C./second. Alloys with scandium in excess of the eutectic compositioncooled normally will have a microstructure consisting of relativelylarge Al₃Sc dispersoids in a finally divided aluminum-Al₃Sc eutecticphase matrix.

The amount of erbium present in the alloys of this invention, if any,may vary from about 0.1 to about 6.0 weight percent, more preferablyfrom about 0.1 to about 4.0 weight percent, and even more preferablyfrom about 0.2 to about 2.0 weight percent. The Al—Er phase diagramshown in FIG. 5 indicates a eutectic reaction at about 6 weight percenterbium at about 1211° F. (655° C.). Aluminum alloys with less than about6 weight percent erbium can be quenched from the melt to retain erbiumin solid solutions that may precipitate as dispersed L1₂ intermetallicAl₃Er following an aging treatment. Alloys with erbium in excess of theeutectic composition can only retain erbium in solid solution by rapidsolidification processing (RSP) where cooling rates are in excess ofabout 10³° C./second. Alloys with erbium in excess of the eutecticcomposition (hypereutectic alloys) cooled normally will have amicrostructure consisting of relatively large Al₃Er dispersoids in afinely divided aluminum-Al₃Er eutectic phase matrix.

The amount of thulium present in the alloys of this invention, if any,may vary from about 0.1 to about 10.0 weight percent, more preferablyfrom about 0.2 to about 6.0 weight percent, and even more preferablyfrom about 0.2 to about 4.0 weight percent. The Al—Tm phase diagramshown in FIG. 6 indicates a eutectic reaction at about 10 weight percentthulium at about 1193° F. (645° C.). Thulium forms Al₃Tm dispersoids inthe aluminum matrix that have an L1₂ structure in the equilibriumcondition. The Al₃Tm dispersoids have a low diffusion coefficient whichmakes them thermally stable and highly resistant to coarsening. Aluminumalloys with less than 10 weight percent thulium can be quenched from themelt to retain thulium in solid solution that may precipitate asdispersed metastable L1₂ intermetallic Al₃Tm following an agingtreatment. Alloys with thulium in excess of the eutectic composition canonly retain Tm in solid solution by rapid solidification processing(RSP) where cooling rates are in excess of about 10³° C./second.

The amount of ytterbium present in the alloys of this invention, if any,may vary from about 0.1 to about 15.0 weight percent, more preferablyfrom about 0.2 to about 8.0 weight percent, and even more preferablyfrom about 0.2 to about 4.0 weight percent. The Al—Yb phase diagramshown in FIG. 7 indicates a eutectic reaction at about 21 weight percentytterbium at about 1157° F. (625° C.). Aluminum alloys with less thanabout 21 weight percent ytterbium can be quenched from the melt toretain ytterbium in solid solution that may precipitate as dispersed L1₂intermetallic Al₃Yb following an aging treatment. Alloys with ytterbiumin excess of the eutectic composition can only retain ytterbium in solidsolution by rapid solidification processing (RSP) where cooling ratesare in excess of about 10³° C. per second. Alloys with ytterbium inexcess of the eutectic composition cooled normally will have amicrostructure consisting of relatively large Al₃Yb dispersoids in afinally divided aluminum-Al₃Yb eutectic phase matrix.

The amount of lutetium present in the alloys of this invention, if any,may vary from about 0.1 to about 12.0 weight percent, more preferablyfrom about 0.2 to about 8.0 weight percent, and even more preferablyfrom about 0.2 to about 4.0 weight percent. The Al—Lu phase diagramshown in FIG. 8 indicates a eutectic reaction at about 11.7 weightpercent Lu at about 1202° F. (650° C.). Aluminum alloys with less thanabout 11.7 weight percent lutetium can be quenched from the melt toretain Lu in solid solution that may precipitate as dispersed L1₂intermetallic Al₃Lu following an aging treatment. Alloys with Lu inexcess of the eutectic composition can only retain Lu in solid solutionby rapid solidification processing (RSP) where cooling rates are inexcess of about 10³° C./second. Alloys with lutetium in excess of theeutectic composition cooled normally will have a microstructureconsisting of relatively large Al₃Lu dispersoids in a finely dividedaluminum-Al₃Lu eutectic phase matrix.

The amount of gadolinium present in the alloys of this invention, ifany, may vary from about 0.1 to about 4 weight percent, more preferablyfrom 0.2 to about 2 weight percent, and even more preferably from about0.5 to about 2 weight percent.

The amount of yttrium present in the alloys of this invention, if any,may vary from about 0.1 to about 4 weight percent, more preferably from0.2 to about 2 weight percent, and even more preferably from about 0.5to about 2 weight percent.

The amount of zirconium present in the alloys of this invention, if any,may vary from about 0.05 to about 1 weight percent, more preferably from0.1 to about 0.75 weight percent, and even more preferably from about0.1 to about 0.5 weight percent.

The amount of titanium present in the alloys of this invention, if any,may vary from about 0.05 to about 2 weight percent, more preferably from0.1 to about 1 weight percent, and even more preferably from about 0.1to about 0.5 weight percent.

The amount of hafnium present in the alloys of this invention, if any,may vary from about 0.05 to about 2 weight percent, more preferably fromabout 0.1 to about 1 weight percent, and even more preferably from about0.1 to about 0.5 weight percent.

The amount of niobium present in the alloys of this invention, if any,may vary from about 0.05 to about 1 weight percent, more preferably fromabout 0.1 to about 0.75 weight percent, and even more preferably fromabout 0.1 to about 0.5 weight percent.

In order to have the best properties for the alloys of this invention,it is desirable to limit the amount of other elements. Specific elementsthat should be reduced or eliminated include no more than about 0.1weight percent iron, about 0.1 weight percent chromium, about 0.1 weightpercent manganese, about 0.1 weight percent vanadium, about 0.1 weightpercent cobalt, and about 0.1 weight percent nickel. The total quantityof additional elements should not exceed about 1% by weight, includingthe above listed impurities and other elements.

Other additions in the alloys of this invention include at least one ofabout 0.001 weight percent to about 0.10 weight percent sodium, about0.001 weight percent to about 0.10 weight calcium, about 0.001 weightpercent to about 0.10 weight percent strontium, about 0.001 weightpercent to about 0.10 weight percent antimony, about 0.001 weightpercent to about 0.10 weight percent barium and about 0.001 weightpercent to about 0.10 weight percent phosphorus. These are added torefine the microstructure of the eutectic phase and the primarymagnesium or lithium morphology and size.

These aluminum alloys may be made by any and all consolidation andfabrication processes known to those in the art such as casting (withoutfurther deformation), deformation processing (wrought processing), rapidsolidification processing, forging, extrusion, rolling, die forging,powder metallurgy and others. The rapid solidification process shouldhave a cooling rate greater that about 10³° C./second including but notlimited to powder processing, atomization, melt spinning, splatquenching, spray deposition, cold spray, plasma spray, laser melting anddeposition, ball milling and cryomilling.

Additional exemplary aluminum alloys of this invention include, but arenot limited to (in weight percent):

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.1-0.35)Sc-(0.2-2.0)Gd;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.1-4)Er-(0.2-2.0)Gd;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.2-6)Tm-(0.2-2.0)Gd;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.2-8)Yb-(0.2-2.0)Gd;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.2-8)Lu-(0.2-2.0)Gd;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.1-0.35)Sc-(0.2-2.0)Y;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.1-4)Er-(0.2-2.0)Y;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.2-6)Tm-(0.2-2.0)Y;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.2-8)Yb-(0.2-2.0)Y;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.2-8)Lu-(0.2-2.0)Y;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.1-0.35)Sc-(0.1-0.75)Zr;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.1-4)Er-(0.1-0.75)Zr;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.2-6)Tm-(0. 1-0.75)Zr;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.2-8)Yb-(0. 1-0.75)Zr;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.2-8)Lu-(0.1-0.75)Zr;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.1-0.35)Sc-(0.1-1.0)Ti;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.1-0.5)Er-(0.1-1.0)Ti;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.2-6)Tm-(0.1-1.0)Ti;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.2-8)Yb-(0.1-1.0)Ti;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.1-4)-Lu-(0.1-1.0)Ti;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.1-0.35)Sc-(0.1-1.0)Hf;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.1-4)Er-(0.1-1.0)Hf;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.2-6)Tm-(0.1-1.0)Hf;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.2-8)Yb-(0.1-1.0)Hf;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.2-8)Lu-(0.1-1.0)Hf;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.1-0.35)Sc-(0.1-0.75)Nb;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.1-4)Er-(0.1-0.75)Nb;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.2-6)Tm-(0.1-0.75)Nb;

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.2-8)Yb-(0.1-0.75)Nb; and

about Al-(2-7)Cu-(0.4-3)Mg-(1-2.5)Li-(0.2-8)Lu-(0.1-0.75)Nb.

Preferred examples of similar alloys to these are alloys with about 3.5to about 6.5 weight percent copper, alloys with about 0.5 to about 2.0weight percent magnesium, and alloys with about 1.0 to about 2.0 weightpercent lithium. Even more preferred exemplary aluminum alloys of thisinvention include, but are not limited to (in weight percent):

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.1-0.25)Sc-(0.2-2.0)Gd;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.2-2)Er-(0.2-2.0)Gd;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.2-4)Tm-(0.2-2.0)Gd;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.2-4)Yb-(0.2-2.0)Gd;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.2-4)Lu-(0.2-2.0)Gd;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.1-0.25)Sc-(0.5-2.0)Y;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.2-2)Er-(0.5-2.0)Y;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.2-4)Tm-(0.5-2.0)Y;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.2-4)Yb-(0.5-2.0)Y;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.2-4)Lu-(0.5-2.0)Y;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.1-0.25)Sc-(0.1-0.5)Zr;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.2-2)Er-(0.1-0.5)Zr;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.2-4)Tm-(0.1-0.5)Zr;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.2-4)Yb-(0. 1-0.5)Zr;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.2-4)Lu-(0.1-0.5)Zr;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.1-0.25)Sc-(0.1-0.5)Ti;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.1-0.5)Er-(0.1-0.5)Ti;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.2-4)Tm-(0.1-0.5)Ti;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.2-4)Yb-(0.1-0.5)Ti;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.1-4)-Lu-(0.1-0.5)Ti;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.1-0.25)Sc-(0.1-0.5)Hf;

about Al-(-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.2-2)Er-(0.1-0.5)Hf;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.2-4)Tm-(0.1-0.5)Hf;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.2-4)Yb-(0.1-0.5)Hf;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.2-4)Lu-(0.1-0.5)Hf;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.1-0.25)Sc-(0.1-0.5)Nb;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.2-2)Er-(0.1-0.5)Nb;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.2-4)Tm-(0.1-0.5)Nb;

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.2-4)Yb-(0.1-0.5)Nb; and

about Al-(3.5-6.5)Cu-(0.5-2)Mg-(1-2)Li-(0.2-4)Lu-(0.1-0.5)Nb.

Although the present invention has been described with reference topreferred embodiments, workers skilled in the art will recognize thatchanges may be made in form and detail without departing from the spiritand scope of the invention.

1. A heat treatable aluminum alloy comprising: about 1.0 to about 8.0weight percent copper; about 0.2 to about 4.0 weight percent magnesium;about 0.5 to about 3.0 weight percent lithium; at least one firstelement selected from the group consisting of about 0.1 to about 0.5weight percent scandium, about 0.1 to about 6.0 weight percent erbium,about 0.1 to about 10.0 weight percent thulium, about 0.1 to about 15.0weight percent ytterbium, and about 0.1 to about 12.0 weight percentlutetium; at least one second element selected from the group consistingof about 0.1 to about 4.0 weight percent gadolinium, about 0.1 to about4.0 weight percent yttrium, about 0.05 to about 1.0 weight percentzirconium, about 0.05 to about 2.0 weight percent titanium, about 0.05to about 2.0 weight percent hafnium, and about 0.05 to about 1.0 weightpercent niobium; and the balance substantially aluminum; wherein thealloy is formed by a process selected from the group consisting ofcasting, deformation processing or rapid solidification processing,followed by heat treating by a solution anneal at a temperature of about800° F. (426° C.) to about 1100° F. (593° C.) for about 30 minutes tofour hours, followed by quenching, and is thereafter aged at atemperature of about 200° F. (93° C.) to about 600° F. (316° C.) forabout two to forty-eight hours.
 2. The alloy of claim 1, wherein thealloy comprises an aluminum solid solution matrix containing a pluralityof dispersed Al₃X second phases having L1₂ structures, wherein Xincludes at least one first element and at least one second element. 3.The alloy of claim 1, further comprising at least one of about 0.001 toabout 0.1 weight percent sodium, about 0.001 to about 0.1 weightcalcium, about 0.001 to about 0.1 weight percent strontium, about 0.001to about 0.1 weight percent antimony, about 0.001 to about 0.1 weightpercent barium, and about 0.001 to about 0.1 weight percent phosphorus.4. The alloy of claim 1, comprising no more than about 1.0 weightpercent total other additional elements not listed therein includingimpurities.
 5. The alloy of claim 1, comprising no more than about 0.1weight percent iron, about 0.1 weight percent chromium, about 0.1 weightpercent manganese, about 0.1 weight percent vanadium, about 0.1 weightpercent cobalt, and about 0.1 weight percent nickel. 6-11. (canceled)12. The heat treatable aluminum alloy of claim 1, wherein the alloy iscapable of being used at temperatures from about −420° F. (−251° C.) upto about 650° F. (343° C.).
 13. A heat treatable aluminum alloycomprising: about 1.0 to about 8.0 weight percent copper; about 0.2 toabout 4.0 weight percent magnesium; about 0.5 to about 3.0 weightpercent lithium; an aluminum solid solution matrix containing aplurality of dispersed Al₃X second phases having L1₂ structures where Xcomprises at least one of scandium, erbium, thulium, ytterbium andlutetium, and at least one of gadolinium, yttrium, zirconium, titanium,hafnium and niobium; the balance substantially aluminum; wherein thealloy is formed by a process selected from the group consisting ofcasting, deformation processing or rapid solidification processing,followed by heat treating by a solution anneal at a temperature of about800° F. (426° C.) to about 1100° F. (593° C.) for about 30 minutes tofour hours, followed by quenching, and is thereafter aged at atemperature of about 200° F. (93° C.) to about 600° F. (316° C.) forabout two to forty-eight hours.
 14. The alloy of claim 13, wherein thealloy comprises at least one of: about 0.1 to about 0.5 weight percentscandium, about 0.1 to about 6.0 weight percent erbium, about 0.1 toabout 10.0 weight percent thulium, about 0.1 to about 15.0 weightpercent ytterbium, about 0.1 to about 12.0 weight percent lutetium,about 0.1 to about 4.0 weight percent gadolinium, about 0.1 to about 4.0weight percent yttrium, about 0.05 to about 1.0 weight percentzirconium, about 0.05 to about 2.0 weight percent titanium, about 0.05to about 2.0 weight percent hafnium, and about 0.05 to about 1.0 weightpercent niobium. 15-19. (canceled)
 20. The alloy of claim 1, furthercomprising at least one of about 0.001 to about 0.1 weight percentsodium, about 0.001 to about 0.1 weight calcium, about 0.001 to about0.1 weight percent strontium, about 0.001 to about 0.1 weight percentantimony, about 0.001 to about 0.1 weight percent barium, and about0.001 to about 0.1 weight percent phosphorus.
 21. The alloy of claim 13,comprising no more than about 1.0 weight percent total other additionalelements not listed therein including impurities.
 22. The alloy of claim21, comprising no more than about 0.1 weight percent iron, about weightpercent chromium, about 0.1 weight percent manganese, about 0.1 weightpercent vanadium, about 0.1 weight percent cobalt, and about 0.1 weightpercent nickel.